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Design and analysis osculating general curved cone waverider

机译:逼近普通弯锥波导管的设计与分析

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Purpose - Waverider has high lift to drag ratio and will be an idea aerodynamic configuration for hypersonic vehicles. But a structure permitting aerodynamic like waverider is still difficult to generate under airframe's geometric constrains using traditional waverider design methods. And furthermore, traditional waverider's aerodynamic compression ability cannot be easily adjusted to satisfy the inlet entrance requirements for hypersonic air-breathing vehicles. The purpose of this paper is to present a new method named osculating general curved cone (OCC) method aimed to improve the shortcomings of traditional waveriders.
机译:目的-Waverider具有高升阻比,将成为高超音速飞行器的理想空气动力学配置。但是,在飞机的几何约束条件下,使用传统的波峰飞行器设计方法仍难以生成像波峰飞行器这样的空气动力学结构。而且,传统的波音赛车的空气动力压缩能力不能轻易地调节以满足高超音速呼吸车辆的进气口要求。本文的目的是提出一种新的方法,称为振荡通用曲线锥(OCC)方法,旨在改善传统波谱仪的缺点。

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